Effects of Orbital Perturbations on Deployment Dynamics of Tethered Satellite System Using Variable-Length Element
Orbital perturbations caused by the space environment will induce deviations compared with the prescribed motion trajectory or dynamic performance of the tethered satellite system (TSS). To comprehensively investigate the effects of the orbital perturbations on the TSS, a precise variable-length ele...
| Hlavní autoři: | , |
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| Médium: | Článek |
| Jazyk: | English |
| Vydáno: |
IEEE
2021-01-01
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| Edice: | IEEE Access |
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| On-line přístup: | https://ieeexplore.ieee.org/document/9344599/ |